N939CC
Bombardier CL-600-2B16 Challenger 601-3A (601-3A)
Canadair Ltd (Bombardier)
8 Hours
Duration of Flight
3430 NM
Range
N/A
Max Speed
Gallery



Basic Information
Airframe
Data valid as of 2023-12-14| Date | From | To | Flight Time | Status |
|---|---|---|---|---|
| 2020-01-09 | N/A | N/A | N/A | ✓ Landed |
| 2014-11-23 | N/A | N/A | N/A | ✓ Landed |
| 2011-10-21 | N/A | N/A | N/A | ✓ Landed |
| 2016-01-01 | N/A | N/A | N/A | ✓ Landed |
AI Summary
Bombardier CL-600-2B16 Challenger 601-3A (601-3A)
Overview
1992 CANADAIR LTD CL-600-2B16 Challenger 601-3A; standard/transport airworthiness; certificate issued 2022-02-07; airworthiness date 2010-06-01; registration expires 2029-02-28.
Specifications
- Engines: 2× GE CF34-3A2 (9220 lbf each)
- Range: 3430 nm
- Cruise: 424 kts
- Seats: 22
- Ceiling: 41000 ft
Operations & Cabin
Typical executive 8–10 place club/forward galley and aft lav; type certificate seating up to 22. Executive leather seating, forward galley, enclosed aft lavatory; cabin length ~28.3 ft, width ~8.2 ft, height ~6.1 ft (typical 601 dimensions). Avionics: Collins Pro Line II (typical for 601-3A retrofits; specific fit varies by airframe)
Model & Market Context
This entry covers airframe N939CC, a Canadair-built Challenger registered in the United States and completed in 1992 with serial number 5124. The airframe is recorded as owned by corporation 601 ASSETS LLC, located in Lighthouse Point, FL, US, and has been associated with corporate asset management rather than an identifiable operating airline. No public record of major registry transfers beyond corporate ownership was provided in the supplied data. The aircraft is noted with an estimated market value of $1,500,000, reflecting its age and configuration.
The airframe is a Bombardier CL-600-2B16 Challenger 601-3A laid out with a typical executive cabin capable of 8–10 place club seating with a forward galley and an aft lavatory, while the type certificate allows seating up to 22. Avionics are listed generically as Collins Pro Line II typical of 601-3A retrofits, with the caveat that specific fit varies by airframe; no unique avionics modifications for this tail were provided. Typical mission profiles for this configuration align with short- to mid-range corporate operations given a cruise speed of 424 kts and a range of 3,430 nm, operating from its owner’s base in Lighthouse Point, FL. Maintenance considerations for this specific aircraft are inferred from its age and engine type but were not itemized in the supplied data.
The Bombardier CL-600-2B16 Challenger 601-3A occupies the mid-size corporate jet niche, offering transcontinental capability with twin GE CF34-3A2 engines and a high single-flight ceiling of 41,000 ft. Competitors in its era and mission class typically include other late-generation heavy light to mid-size business jets; buyer demand and charter interest for a 1992 Challenger are influenced by cabin layout, avionics retrofits such as Collins Pro Line II, and lifecycle maintenance status. Resale and maintenance considerations for this airframe are shaped by its age, the availability of service for CF34 family engines, and the recorded valuation of $1,500,000.
Aircraft Comparison
| Parameter | N939CC | N118MT | N141RD |
|---|---|---|---|
| Serial Number (MSN) | 5124 | 5077 | 1041 |
| Year Manufactured | 1992 | 1990 | 1982 |
| Duration of Flight | 8 Hours | 8 Hours | 7 Hours |
| Range | 3430 NM | 3365 NM | 2909 NM |
| Max Speed | N/A | 459 MPH | 458 MPH |
| Aircraft Class | Over 20,000lbs | Over 20,000lbs | Over 20,000lbs |
| Service Ceiling | 41000 ft | 41000 ft | 41000 ft |
| Max Passengers | 22 | 22 | 13 |
| Cabin Comfort | No items found. | No items found. | No items found. |